Accession Number : ADA265275


Title :   Theoretical Investigation of 3-D Shock Wave - Turbulent Boundary Layer Interactions


Descriptive Note : Interim rept. 1 Mar-30 Sep 92,


Corporate Author : RUTGERS - THE STATE UNIV NEW BRUNSWICK NJ DEPT OF MECHANICAL AND AEROSPACE ENGINEERING


Personal Author(s) : Knight, Doyle D


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/a265275.pdf


Report Date : Nov 1992


Pagination or Media Count : 59


Abstract : The research concerns the understanding of 3-D shock wave/turbulent boundary-layer interactions. The research effort during the current period focused on the following areas: (a) the 3-D double fin ( crossing shock ) interaction at Mach 8.3 for symmetric 15 deg fins, (2) the 3-D crossing shock interaction at Mach 4 for symmetric 15 deg fins, and (3) the 3-D tripe ( triple shock ) interaction at Mach 8.3 for 10 deg fins


Descriptors :   *INTERACTIONS , *SHOCK WAVES , *TURBULENT BOUNDARY LAYER , *THREE DIMENSIONAL FLOW , *HYPERSONIC FLOW , YAW , AIR FORCE RESEARCH , VORTICES , NAVIER STOKES EQUATIONS , SHOCK TESTS


Subject Categories : Fluid Mechanics


Distribution Statement : APPROVED FOR PUBLIC RELEASE